ELECTRON R/B (1), 68800

Orbit data source: Space-Track

ELECTRON R/B (1), 68800 is space debris in SSO originally from a launch on Thu, 23 Apr 2026 UTC launched from the Rocket Lab Launch Complex (RLLC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
68800, 2026-088J
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Rocket Lab
Mission
Spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
2026-04-23 (22 hours ago)
Launch vehicle
Unknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 ELECTRON R/B (1)
1 68800U 26088J   26113.86170093  .00637055  22657-5  47113-3 0  9995
2 68800  97.4982 264.6236 0273620 210.4209 148.0935 15.69511433   110
Epoch: 2026-04-23T20:40Z
TLE epoch observation values (Epoch: 2026-04-23T20:40:50.960Z)
Latitude
-0.00001°
Longitude
102.50857°
Altitude
521.368 km
Speed
7.513 km/s
True Right ascension
17h 38m 29s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
17:09:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.488 km
Perigee altitude
172.904 km
Semi-major axis
6,735.333 km
Eccentricity
0.02736
Inclination
97.4982°
RAAN
264.6236°
Arg. of periapsis
210.4209°
True anomaly
149.70368°
Mean anomaly
148.0935°
Eccentric anomaly
148.90321°
Mean motion
3.92649 °/min
Orbital period
91.68 mins
BSTAR
0.00047113
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